# Service difficulty reports: N24224

A list on [N24224](https://openairdocs.org/aircraft/N24224.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 93 reports

- [SDR CALA2026100520117](https://openairdocs.org/sdr/CALA2026100520117.md): Wire Harness · faulted · Sep 27, 2026 · N24224 · Boeing 737824 · Light System Wiring
  > EMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - SEAT MOUNTED FLOOR PROXIMITY LIGHT AT 34ABC INOP REQUESTING MEL RELIEF, ALL MONUMENT MOUNTED LIGHTS OPERATIONAL, ALL FLOODLIGHTS AND EXIT IDENTIFIER LIGHTS OPERATIONAL, ALL OTHER SEAT MO
- [SDR CALA2026092919985](https://openairdocs.org/sdr/CALA2026092919985.md): Light · no discrepancy · Sep 27, 2026 · N24224 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS OPERATIONAL CHECK - DOOR 2R EMERGENCY SLIDE LIGHT INOP. PERFORMED OPS CHECK DOOR 2R EMERGENCY SLIDE LIGHT INOP OPS CHECKS GOOD IAW AMM 33-51-00
- [SDR CALA2026091119380](https://openairdocs.org/sdr/CALA2026091119380.md): Lamp · faulted · Sep 7, 2026 · N24224 · Boeing 737824 · Emergency Lighting
  > LIGHT OVER FWD RT EMERGENCY OVERWING EXIT WAS ILLUMINATED & FLASHING RED IN FLT. LIGHT IS NOW COMPLETELY OUT ON GROUND. EMERGENCY EXIT SIGN WORKS NORMAL, UPPER DOOR BULB IS INOPERATIVE. R & R OVERWING EXIT LAMP. OPS CHKD GOOD. REF AMM 33-21-00-960-806.
- [SDR CALA2026071217724](https://openairdocs.org/sdr/CALA2026071217724.md): Door · out of limits · Jul 10, 2026 · N24224 · Boeing 737824 · Passenger/Crew Doors
  > AFT ENTRY LIGHT ON DOOR HANDLE UNABLE TO CLOSE OPENED AT ALTITUD PERFORMED AFT ENTRY DOOR SYSTEM TEST REF AMM 52-13-00-700-805. INTERIOR DOOR HANDLE CLOSES AND OPENS WITHIN TORQUE RANGE SPECIFIED IN AMM. NO DEFECTS FOUND AT THIS MOMENT. PERFORMED CABIN PRESSUR
- [SDR CALA2026031114506](https://openairdocs.org/sdr/CALA2026031114506.md): Actuator · leaking · Mar 9, 2026 · N24224 · Boeing 737824 · Landing Gear Retraction/Extension System
  > NOSE DROPPED AFTER GEAR HANDLED MOVED FROM UP TO OFF. CREW ADVISED -FOLLOWED QRH. CYCLED THE GEAR BACK UP AND GEAR HANDLE REMAINS IN THE UP POSITION. ALL INDICATIONS NORMAL AND NLG REMAINED UP. ON DEBRIEF OF PILOT, ENTIRE NLG DROPPED NOT JUST THE NOSE OF AC
- [SDR CALA2025122112283](https://openairdocs.org/sdr/CALA2025122112283.md): Transmitter · faulted · Dec 19, 2025 · N24224 · Boeing 737824 · Trailing Flap Position Indicating System
  > FLAPS STOPED AT 2, NO TRAILING EDGE FLAPS UNTIL ALT FLAPS. SHOWS LEFT TE FLAP POSITION TRANSMITTER LAGGING BAD. REMOVED & REPLACED THE LT FLAP TRANSMITTER & PERFORMED ALL TESTS IAW AMM 27-58-01. NO FAULT NOTED.
- [SDR CALA2025112811539](https://openairdocs.org/sdr/CALA2025112811539.md): Slide · faulted · Nov 24, 2025 · N24224 · Boeing 737824 · Escape Slide
  > R1 DOOR EMERGENCY EXIT SLIDE HANGS OUT EXCESSIVELY GIRT BAR AT R1 DOOR SLIDE STOWED PROPERLY. VISUAL INSPECTION SHOWS PROPER MOUNTING WITH NO LOOSE COVER. GIRT BAR SLIDE ATTACHMENT SHOWES NO INTERFERENCE.
- [SDR CALA2025091208832](https://openairdocs.org/sdr/CALA2025091208832.md): Support Beam · damaged · Sep 11, 2025 · N24224 · Boeing 737824 · Fuselage Miscellaneous Structure
  > LOWER SUPPORT BEAM LOWER CORD NEXT TO PANEL 192DR HAS DAMAGE FROM DOOR LATCH. REMOVED PREVIOUSLY REPAIRED DAMAGED PARTS STRAP AND FILLER REF SRM 51-40-02. REPLACED FILLER AND STRAP FROM PREVIOUS REPAIR WITH SRM 57-10-13-2R-3.
- [SDR CALA2025091108760](https://openairdocs.org/sdr/CALA2025091108760.md): Slide · no discrepancy · Sep 9, 2025 · N24224 · Boeing 737824 · Escape Slide
  > DOOR 1R - SLIDE PRESSURE GUAGE IS IN THE RED. DOOR 1R SLIDE PRESSURE GAUGE WITHIN LIMITS AMM REFERENCE: TASK 25-66-01-200-801
- [SDR CALA2025090908654](https://openairdocs.org/sdr/CALA2025090908654.md): Cover · unsecure · Sep 5, 2025 · N24224 · Boeing 737824 · Escape Slide
  > SLIDE RAFT COVER NOT SECURE CREW REPORTS CONCERN ABOUT SLIDE COVER (BUSTLE) NOT SECURE AT DOOR 1R. VERIFIED SECURITY SECURITY OF COVER FASTENERS AND COVER SECURE WITH PAWL ENGAGED. REF AMM TASK 25-66-01-400-803. OKAY TO FONTINUE.
- [SDR CALA2025061005418](https://openairdocs.org/sdr/CALA2025061005418.md): Unknown · odor · Jun 9, 2025 · N24224 · Boeing 737824 · Air Distribution System
  > FLIGHT ATTENDANTS REPORT ELECTRIC SMELL FROM BACK AFTER LANDING AFTER SPEAKING WITH FLT ATT IN AFT GALLEY THERE WAS INDENTIFIABLE SOURCE OF ELECT SMELL, OVENS AND COFFEE MKRS WERE OFF NO POPPED BREAKERS, GALLEY LIGHTS ALL CKED GOOD, OK TO CONTINUE
- [SDR CALA2025040203451](https://openairdocs.org/sdr/CALA2025040203451.md): Skin Panel · damaged · Mar 29, 2025 · N24224 · Boeing 737824 · Fuselage Main, Plate/Skin
  > LOWER FWD FUSELAGE LH SIDE EXTERNAL SKIN HAS DAMAGE JUST OUTBD OF FWD E&E FWD FRAME CUTOUT 31 INCHES AFT OF 178 BULKHEAD MARKED WITH TAPEDAMAGE MEASURES OUT A TOTAL DIAMETER OF 1.5 INCHES AND HAS A DEPTH OF.032". CENTER OF DAMAGE IS LOCATED 8" BELOW FACTORY L
- [SDR CALA2025040103394](https://openairdocs.org/sdr/CALA2025040103394.md): Skin · cracked · Mar 28, 2025 · N24224 · Boeing 737824 · Fuselage Main, Plate/Skin
  > INSTALL REPAIR PARTS REF AVO 14374 REV A THIS IS A STEP IN A MAJOR REPAIR, REQUIRES INSPECTION, RII INSTALLED REPAIR PER AVO14374 WITH NO DEVIATIONS TO AVO. REPAIR WAS INSTALLED USING AVO14374 REV C. ACCOMPLISHED RII REQUIREMENTS FOR FUSELAGE REPAIR IN REF TO
- [SDR CALA2025031102702](https://openairdocs.org/sdr/CALA2025031102702.md): Window Frame · cracked · Mar 9, 2025 · N24224 · Boeing 737824 · Fuselage Main, Structure
  > AS PER EA 5310-04554 REV D OP 003 - COCKPIT LH NO 1 WINDOW FRAME UPPER AFT CORNER CRACK AT RADIUS. REF AAR N/R 9939578. SDR REPORTING FOR MAJOR REPAIR. ACCOMPLISHED EA 5310-04554 REV D OP 003-LH NO 1 WINDOW FRAME PERMANENT REPAIR/ PREVENTATIVE MODIFICATION WHI
- [SDR CALA2025031102701](https://openairdocs.org/sdr/CALA2025031102701.md): Window Frame · cracked · Mar 9, 2025 · N24224 · Boeing 737824 · Fuselage Main, Structure
  > AS PER EA 5310-04554 REV D OP 004 - COCKPIT RH NO 1 WINDOW FRAME CRACK AT UPPER OUTB CORNER RADIUS. REF AAR N/R 9939591. MAJOR REPAIR. ACCOMPLISHED EA 5310-04554 REV D OP 004-RH #1 WINDOW FRAME PERMANENT REPAIR/ PREVENTATIVE MODIFICATION WHICH REMOVES THE #1 W
- [SDR CALA2025031002659](https://openairdocs.org/sdr/CALA2025031002659.md): Skin · corroded · Mar 9, 2025 · N24224 · Boeing 737824 · Fuselage Main, Plate/Skin
  > AFT OF FWD CARGO COMPARTMENT A/C BAY BILGE SKIN CHECK FUS CUTOUT SURROUNDING AREA CORROSION BETWEEN STA 520 AND STA 540. REF AAR N/R 9939574.
- [SDR CALA2025031002662](https://openairdocs.org/sdr/CALA2025031002662.md): Angle · corroded · Mar 7, 2025 · N24224 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA STA 1006 LBL 30 Z ANGLE HAS CORROSION. REF AAR N/R 9939014.FOUND Z-ANGLE WITH EXFOLIATED CORROSION OUT OF LIMITS, REMOVED AND INSTALLED NEW Z-ANGLE IN REF TO SRM 51-40-02-0G-0 SRM 53-70-51-1A-1 AND DWG 147AG700.
- [SDR CALA2025031002660](https://openairdocs.org/sdr/CALA2025031002660.md): Web · corroded · Mar 7, 2025 · N24224 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT BILGE S-25L CORRODED AT I/B FLANGE AND INNER WEB BETWEEN STA 827 AND STA 847. REF AAR N/R 9939609. SFR ENTRY INFO ONLY ACCOMPLISHED THREE SPLICE REPAIRS TO STR 25L BETWEEN STA 807 AND STA 867 AS PER EC/RA 5360-01937. NO FURTHER ACTION REQ
- [SDR CALA2025031002656](https://openairdocs.org/sdr/CALA2025031002656.md): Support Fitting · damaged · Mar 6, 2025 · N24224 · Boeing 737824 · Doors
  > FWD ENTRY DOOR BODY TORQUE TUBE UPPER CUTOUT SUPPORT FITTING GUIDE PLATE HAS ELONGATED HOLE. REF AAR NR9939408.REMOVED AND REPLACED NEW SUPPORT FITTING (UPPER HINGE BOX) IN REF SRM51-40-02-0G-0 AND DWG141A8180. REMOVED AND REPLACED NEW SUPPORT FITTING (UPPER
- [SDR CALA2025031002655](https://openairdocs.org/sdr/CALA2025031002655.md): Bulkhead Web · cracked · Mar 5, 2025 · N24224 · Boeing 737824 · Fuselage Main, Bulkhead
  > MAIN LANDING GEAR WHEEL WELL AREA STA 663 LBL 24 VAPOR WEB IS CRACKED. (REF AAR N/R 9939252) ACCOMPLISHED INTERIM PATCH REPAIR AT STA 663 LBL 24 MAIN WHEEL VAPOR VARRIER IN REF TO SRM 57-10-10-2R-2. THIS INTERIM REPAIR REQUIRES A DVI INSPECTION EVERY 3,000 FLI
- [SDR CALA2025031002652](https://openairdocs.org/sdr/CALA2025031002652.md): Skin · cracked · Mar 5, 2025 · N24224 · Boeing 737824 · Leading Edge Devices
  > L/W MOVEABLE L/E SLAT 1 LOWER L/E SKIN CRACKED AT FASTNER HEAD AT ACTUATOR ATTACHED RIB MKD DOT 018 REF AAR N/R 9938796 ACCOMPLISHED PERMANENT REPAIR AT L/W ROTABLE L/E SLAT 1 LOWER L/E SKIN AS PER B737 SRM 57-42-012R-8 ALTERNATIVE 1 FIGURE 202 SHEET 1 WORK AC
- [SDR CALA2025031002650](https://openairdocs.org/sdr/CALA2025031002650.md): Skin · corroded · Mar 5, 2025 · N24224 · Boeing 737824 · Fuselage Main, Plate/Skin
  > LEFT WING UNDER WING TO BODY FAIRING FUS SPOT EXFOLIATED CORR. BELOW ATTACHED ANGLE S-22L STA 540 REF AAR N/R 9939235
- [SDR CALA2025030702609](https://openairdocs.org/sdr/CALA2025030702609.md): Scuff Plate · corroded · Mar 5, 2025 · N24224 · Boeing 737824 · Fuselage Miscellaneous Structure
  > L1 DOOR LOWER CUTOUT SCUFF PLATE CAVITY, CHORD LOWER SILL SURFACE EXCESSIVE CORROSION (EXFOLIATION) NOTED REF AAR N/R 9939012 REMOVED AND REPLACED L1 DOOR CUTOUT SCUFF PLATE CHORD LOWER SILL AS PER B737 SRM 51-40-02-0G-0 AND DRWG 141A8100 SHEET 3 WORK ACCOMPLI
- [SDR CALA2025030702607](https://openairdocs.org/sdr/CALA2025030702607.md): Skin · cracked · Mar 5, 2025 · N24224 · Boeing 737824 · Leading Edge Devices
  > RIGHT WING MOVEABLE SLAT # 5 LOWER L/E SKIN ACTUATOR SUPPORT RIB SEVERAL LOOSE FASTENERS AND APPEAR CRACKED AROUND FASTENERS HOLES MKD DOT 082 REF AAR N/R 9939338 ACOOMPLISHED SLAT #5 LOWER SKIN REPAIRED REF SRM 57-42-01-2R-8.
- [SDR CALA2025030702606](https://openairdocs.org/sdr/CALA2025030702606.md): Plate · corroded · Mar 5, 2025 · N24224 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CORROSION L1 DOOR LOWER CUTOUT SCUFF PLATE CAVITY, INNER CHORD ANGLE SURFACE EXCESSIVE CORROSION (EXFOLIATION) NOTED REF AAR N/R 9939011 REMOVED AND REPLACED L1 DOOR CUTOUT SCUFF PLATE INNER CHORD ANGLE AS PER B737 SRM 51-40-02-0G-0 AND DWG 141A8110 SHEET 3REM
- [SDR CALA2025030402573](https://openairdocs.org/sdr/CALA2025030402573.md): Floor Support · cracked · Mar 3, 2025 · N24224 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AT AFT HOLE UPPER CHORD BETWEEN STA 294.5 AND 312 RBL 33. REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL AT FWD CABIN WET AREA STA 294.5-312 RBL 33 IAW B-737 SRM 51-40-02-0G-0 AND DWG NUMBER 141A5400.
- [SDR CALA2025022800462](https://openairdocs.org/sdr/CALA2025022800462.md): Stringer · corroded · Feb 26, 2025 · N24224 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > AREA OF AFT FWD CARGO COMPARTMENT AT STR 27L STA 540 CORROSION FOUND REF AAR N/R 9939788 ACCOMPLISHED PERMANENT STRINGER SPLICE REPAIR ACCORDING ECRA 5330-07464 NO FURTHER ACTON REQUIRED WORK ACCOMPLISHED BY V936290 ACCOMPLISHED PERMANENT STRINGER SPLICE REPAI
- [SDR CALA2025022700461](https://openairdocs.org/sdr/CALA2025022700461.md): Stringer · corroded · Feb 26, 2025 · N24224 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > ARA OF FWD CARGO COMPT STRINGER 27R IS CORRODED AT BS 540 REF AAR N/R 9939793 ACCOMPLISHED PERMANENT REPAIR ACCORDING TO ECRA 5330-07463 NO FURTHER ACTION REQUIRED.
- [SDR CALA2025022700460](https://openairdocs.org/sdr/CALA2025022700460.md): Support Fitting · corroded · Feb 26, 2025 · N24224 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD ENTRY L-1 DOOR BODY TORQUE TUBE LOWER HINGE CUTOUT SUPPORT HOLE CORRODED REF AAR N/R 9939407 REMOVED AND DISCARDED DAMAGEDE LOWER HINGE BOX BODY TORQUE TUBE LOWER HINGE CUTOUT SUPPORT LOCATED AND DRILLED HOLES ON NEW LOWER HINGE BOX AND INSTALLED AS PER SR
- [SDR CALA2025022600451](https://openairdocs.org/sdr/CALA2025022600451.md): Rib · cracked · Feb 25, 2025 · N24224 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONTAL STAB FRONT SPAR L/E FAIRING INT RIB # 18 CRACKED MKD DOT 246. (REF AAR N/R 9939746)(FOR ESFR PURPOSES)
- [SDR CALA2025022600449](https://openairdocs.org/sdr/CALA2025022600449.md): Cusp Web · corroded · Feb 25, 2025 · N24224 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN L/H SIDEWALL LOWER CUSP WEB CORR. BETWEEN STA 500 AND 500A MKD DOT 101. (REF AAR N/R 9939389)(FOR ESFR PURPOSES)
- [SDR CALA2025021900384](https://openairdocs.org/sdr/CALA2025021900384.md): Window Frame · cracked · Feb 15, 2025 · N24224 · Boeing 737824 · Fuselage Main, Structure
  > R/H WINDSHILD # 1 FRAME FITTING SPLICE HAS A CRACK DOT 253-039. (REF AAR N/R 9939821) REMOVED AND REPLACED FRAME FITTING SPLICE AT RH WINDSHIELD #1 AS PER B737 SRM 51-40-02-05-0 PARAGRAPH 7.D.
- [SDR CALA2025021400359](https://openairdocs.org/sdr/CALA2025021400359.md): Stringer · corroded · Feb 13, 2025 · N24224 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > AFT OF FWD CARGO COMPMT A/C BAY BILGE S-28R CORR BETWEEN STA 520 AND STA 540 REF AAR N/R 9939704
- [SDR CALA2025021400358](https://openairdocs.org/sdr/CALA2025021400358.md): Stringer · corroded · Feb 13, 2025 · N24224 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > AFT OF FWD CARGO COMP A/C BAY BILGE S-28L CORROSION BETWEEN STA 520 AND 540 REF AAR N/R 9939752
- [SDR CALA2025020600311](https://openairdocs.org/sdr/CALA2025020600311.md): Floorbeam · corroded · Feb 4, 2025 · N24224 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT CABIN WET AREA STA 947 RBL 50 FLOOR BEAM HAS CORROSION (REF AAR N/R 9939022)
- [SDR CALA2025020200261](https://openairdocs.org/sdr/CALA2025020200261.md): Structure · corroded · Feb 2, 2025 · N24224 · Boeing 737824 · Passenger/Crew Doors
  > L2 DOOR ENTRY INNERCHORD HAS CORROSION. REMOVE CORROSION AT L-2 DOOR INNER CHROD. EVALUATED CORROSION REMOVAL FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED L-2 DOOR INNERCHORD. IN REF TO SRM 51-10-02-0G-0, SRM 53-70-14-1A-1 AND SRM 51-40-02-0G-0. DWG #147AB
- [SDR CALA2025020400284](https://openairdocs.org/sdr/CALA2025020400284.md): Floor Support · corroded · Jan 29, 2025 · N24224 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL UPPER CHORD HAS PITTING CORR. SPOT. AT LBL 12 BETWEEN STA 294.5 AND 312 MKD DOT 176 REF AAR N/R 9939583
- [SDR CALA2025012900226](https://openairdocs.org/sdr/CALA2025012900226.md): Floorbeam · corroded · Jan 25, 2025 · N24224 · Boeing 737824 · Fuselage Main, Floor Beam
  > FWD WET AREA FLOOR STRUCTURE, PANEL BREAK BTW STA 312 - 328 LBL 12 IN. AROUND 2EA. FATENER HOLES CORROSION FOUND DOT 223-014. (REF AAR N/R 9939006) REMOVED AND REPLACED PANEL BREAK AT FWD WET AREA FLOOR STRUCTURE BTW STA 312-328 LBL 121N PER B737-800 REF: SRM
- [SDR CALA2025012900225](https://openairdocs.org/sdr/CALA2025012900225.md): Floor Support · cracked · Jan 25, 2025 · N24224 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD WET AREA FLOOR STRUCTURE, INTERCOSTAL BTW STA 312 - 328 LBL 47 UPPER SURFACE NEAR FASTENER HOLE CRACK NOTED DOT 223-036. (REF AAR N/R 9939433) REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA BTW STA 312-328 LBL 47 IAW B737 SRM 57-40-02-0G-0 AND DWG 141A5
- [SDR CALA2025012900224](https://openairdocs.org/sdr/CALA2025012900224.md): Stringer Clip · damaged · Jan 25, 2025 · N24224 · Boeing 737824 · Fuselage Main, Attach Fittings
  > MAIN CABIN STRINGER 10R CLIP IS CRACKED AT STA 277. (REF AAR N/R 9939337) REMOVED DAMAGED STRINGER CLIP, FABRICATED NEW STRINGER CLIP SHEET 16 PN 141A1250-71 FROM A17075-T62 EXT BAC149-852 IAW DWG 141A1250 SHEET 71 AND INSTALLED AS PER SRM 51-40-02-0G-0 AND BO
- [SDR CALA2024112601298](https://openairdocs.org/sdr/CALA2024112601298.md): Battery Pack · no test · Nov 24, 2024 · N24224 · Boeing 737824 · Emergency Lighting
  > TAIL EMERGENCY LIGHT RIGHT HEAD SIDE INOP REMOVED AND REPLACED LAMP IN EMEGENCY LIGHT NO HELP SUSPECT POWER SUPPLY D717-02-001 REPLACED EMERGENCY BATTERY PACK M1672 WITH NEW BATTERIES. OPS CHK WAS GOOD.
- [SDR CALA2024082000458](https://openairdocs.org/sdr/CALA2024082000458.md): Brake · worn · Aug 16, 2024 · N24224 · Boeing 737824 · Landing Gear Brake System
  > RIGHT INSIDE MAIN BRAKE WEAR INDICATOR WORN BEYOND LIMITS FOUND # 3 MAIN LANDING GEAR BRAKE ASSY WITH ONE BRAKE ROTOR COMPLETELY MISSING / SHATTERED, REMOVED AND REPLACED BRAKE ASSY, INSPECTED AXEL WITH NO DAMAGE NOTED.PER AMM 32-41-41. PARTS USED: 60-3241-
- [SDR CALA2024081902235](https://openairdocs.org/sdr/CALA2024081902235.md): Brake · failed · Aug 16, 2024 · N24224 · Boeing 737824 · Landing Gear Brake System
  > RIGHT INSIDE MAIN BRAKE WEAR INDICATOR WORN BEYOND LIMITS FOUND # 3 MAIN LANDING GEAR BRAKE ASSY WITH ONE BRAKE ROTOR COMPLETELY MISSING / SHATTERED. REMOVED AND REPLACED BRAKE ASSY, INSPECTED AXEL WITH NO DAMAGE NOTED.PER AMM 32-41-41.
- [SDR CALA2024071900261](https://openairdocs.org/sdr/CALA2024071900261.md): Warning Message · illuminated · Jul 16, 2024 · N24224 · Boeing 737824 · Central Warning
  > TAKEOFF CONFIG WARNING ACTIVATED ON TAKEOFF. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. COMPLETED TAKEOFF WARNING REPORT FAULTS - FAULT ISOLATION PER FIM 31-51 TASK 822. NO FAULTS FOUND. COMPLETED TAKEOFF WA
- [SDR CALA2024041501087](https://openairdocs.org/sdr/CALA2024041501087.md): Panel · missing · Apr 11, 2024 · N24224 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > PDA 1 ON WALKAROUND, FOUND PANEL 343FB MISSING. REF IPC 55-10-00-12 ITEM 625. P/N 185A1702-12 DOES NOT BREAK TO M&E. MFG PN DOES BREAK TO M&E 29-5510-3-0184. REF AMM 55-10-11-400-801 FOR INSTALLATION OF PANEL REPLACED MISSING PANEL ON R/H T/E OF STAB 343FB W
- [SDR CALA2023042101208](https://openairdocs.org/sdr/CALA2023042101208.md): Transducer · inoperative · Apr 21, 2023 · N24224 · Boeing 7378 · Brake Anti-Skid Section
  > W/GEAR HANDLE IN UP POS ANTI SKID INOP LIGHT ON. W GEAR HANDLE I N OFF AND DN ANTI SKID LIGHT OFF REMOVED AND REPLACED #2 MLG ANTI-SKID TRANSDUCER IAW AMM 32-42-11. PERFORMED OPS CHECK W/ REF TO AMM 32-42-00 OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. PARTS USED
- [SDR CALA2022020200297](https://openairdocs.org/sdr/CALA2022020200297.md): Fire Loop · damaged · Feb 1, 2022 · N24224 · Boeing 737824 · Fire Detection
  > ENG1 FIRE LIGHT ILLUMINA TED THEN EXTINGUISHED. FOUND 3 OUT OF THE 4 CORE ELEMENTS CHECKING BAD. REMOVED AND REP LACED L/H AND R/H CORE ASSY WHICH CONTAIN BOTH A&B ELEMENTS. ALSO FOUND B LOOP CORE HARNESS OPEN. REMOVED AND REPLACED B LOOP CO RE HARNESS. OPS CH
- [SDR CALA2021120602268](https://openairdocs.org/sdr/CALA2021120602268.md): Connector · broken · Dec 6, 2021 · N24224 · Boeing 737824 · Smoke Detection
  > ENG FIRE WARN NO1 ENG PAGE LOCKED PAGE UNLOCKED ACCOMPLISHED ENGINE-APU FIRE DETECTION CONTROL MODULE BITE RETERMINATED. VERIFIED NORMAL OPERATION WITH ENGINE IDLE RUN. PROCEDURE REF FIM 26-10-801. FOUND 1 LOOP B LOW DET RESIS. FAULT ACCOMPLISHED ENGINE LOW DE
- [SDR CALA2021100101761](https://openairdocs.org/sdr/CALA2021100101761.md): Fastener · missing · Oct 1, 2021 · N24224 · Boeing 7378 · Wing Structure
  > PDA 3 1 EACH FASTENER MISSING ON LEFT WING PANEL 551DT. ADDED PHOTO OF PANEL 551DT. INSTALLED 1 EA FASTENER ON L/H WING PANEL 551DT PER AMM 57-15-00-400-801.
- [SDR CALA2021100101756](https://openairdocs.org/sdr/CALA2021100101756.md): Fastener · missing · Oct 1, 2021 · N24224 · Boeing 7378 · Wing Structure
  > PDA 3 FASTENER MISSING 1 EACH ON LEFT WING PANEL 551ET. ADDED PHOTO. PANEL 551ET INSTALLED 1 EA FASTENER ON L/H WING PANEL 551ET PER AMM 57-15-00-400-801.

Next page: https://openairdocs.org/aircraft/N24224/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N24224' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N24224/reports

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